Embraer EMB-135ER
Service difficulty reports · 465
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'EMB135ER' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE aircraft_model_key = 'EMB135ER' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C2XA06CL034Fuel Control · leakingCLE FLIGHT NR 2592, THE CREW REPORTED A STRONG FUEL SMELL WHEN STARTING THE APU. MAINTENANCE INSPECTED AND PLACED THE APU ON MEL IAW 49-00-00. CLE FLIGHT NR 3235 MAINTENANCE ENTRY FOR CLEARING MEL. MAINTENANCE REMOVED AND REPLACED THE APU FUEL CONTROL UNIT.SDR C2XA06BT013Tire · damagedCREW REPORTED, LOUD VIBRATION AND BUZZING SOUND COULD BE HEARD DURING FLT, CONTACTED COMPANY ON FREQUENCY THEN INFORMED THAT WE HAD LOST A TIRE ASSY ON TAKEOFF, LT NR 1 MAIN TIRE MISSING ON POST FLT. A/C LANDED UNEVENTFULLY. MX R & R NR 1 & 2 BRAKE ASSEMBLIESDR C2XA06CL032Switch · faultyCLE FLIGHT 2501 THE CREW REPORTED A VERY LOUD NOISE FROM THE FORWARD SECTION OF THE AIRCRAFT. MAINTENANCE INSPECTED AND FOUND THE NOSE GEAR DOORS WOULD NOT CLOSE AFTER GEAR RETRACTION. THE NOSE GEAR DOOR SEQUENCE PROXIMITY SWITCH WAS REPLACED. OPERATIONAL CSDR C2XA06CL028Switch · faultyCLE - THE CREW REPORTED RIGHT GEAR NO INTRANSIT INDICATION WHEN GEAR WAS RETRACTED. MAINTENANCE INSPECTED AND REPLACED THE RIGHT GEAR UPLOCK PROXIMITY SWITCH. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL025Terminal · burnedCLE FLIGHT 2944, THE CREW REPORTED A VERY STRONG ELECTRICAL BURNING SMELL IN THE COCKPIT ANYTIME ANT-ICE WAS ON. MAINTENANCE INSPECTED AND FOUND THE -P- TERMINAL ON THE RIGHT WINDSHIELD BURNT. THE RIGHT WINDSHIELD WAS REPLACED. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL024Lamp · inoperativeDURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE LAMP. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL022Windshield · faultyCLE FLIGHT 2453 THE CREW REPORTED SMOKE VISIBLE FROM CAPTAIN'S LOWER WINDSHIELD. MAINTENANCE INSPECTED AND REPLACED THE CAPTAINS WINDSHIELD. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL012Splice · looseDURING ROUTINE MAINTENANCE THE SERVICE DOOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE INSPECTED AND REPLACED THE SPLICE SP9043 AT THE EXIT IDENTIFIER SIGN AT THE SERVICE DOOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA06CL009Pdu · failedCLE FLIGHT 2056 - THE CREW REPORTED A -FLAP FAIL- MESSAGE ON THE EICAS UPON SELECTING FLAPS -22- DEGREES. FLAPS WERE STUCK AT THE -18- DEGREE POSITION. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THESDR C2XA06CL007Duct · looseCLE FLIGHT 2578 - THE CREW REPORTED A BURNING RUBBER SMELL FROM THE NR 2 PACK. MAINTENANCE INSPECTED AND REINSTALLED DUCT UNDER FLOORBOARD ON THE NR 2 PACK. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05SH135Floor Support · corrodedSHV - DURING C-CHECK MAINTENANCE, FOUND CENTER OMEGA BEAM CORRODED AT FRAME 20. MAINTENANCE REMOVED AND REPLACED CENTER OMEGA BEAM AT FRAME 20 TO FRAME 23 IAW EMB 135 SRM 51-40-02. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA05CL092Charger · burnedCLE - THE CREW REPORTED A ELECTRICAL BURNING SMELL IMMEDIATELY AFTER TAKEOFF. THE AIRCRAFT RETURNED TO CLE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE FORWARD FLIGHT ATTENDANT FLASHLIGHT AND CHARGER ASSEMBLY. ALSO REPLACED THE CEILING LIGHT ABOVE SEASDR C2XA05TY057Connector · looseTYS - ON CLIMB THE CREW GOT A ICAS MESSAGE THAT THE WING ANTI-ICE FAIL, CREW RETURN TO BLOCK AND MAINTENANCE FOUND A PUSH PIN ON A CONNECTOR LOOSE. MAINTENANCE REINSERTED THE PIN AND OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED TO SERVICE.SDR C2XA05CL077Acm · defectiveCLE FLIGHT NR 2268, CREW REPORTED, SAW AND SMELLED SMOKE IN THE AIRCRAFT WITH PACK NR 1 ON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED NR 1 AIR CYCLE MACHINE. OPERATIONAL CHECKS WERE REPORTED GOOD.SDR C2XA05CL065Bulb · inoperativeDURING ROUTINE MAINTENANCE, THE EMERGENCY CEILING LIGHT AT ROW 6 WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05CL040Bellcrank · wornCREW REPORTED MAIN CABIN DOOR HARD TO OPEN. MX INSP AND REPLACED ACTUATING CAM BELLCRANK AND BUSHING. OPS CHECK GOOD.SDR C2XA05CL039Bar · bindingCLE FLIGHT 2944 THE CREW REPORTED THE MAIN CABIN DOOR WAS DIFFICULT TO OPEN. MAINTENANCE INSPECTED AND ADJUSTED THE UPPER AND LOWER STABILIZER BARS OF THE MAIN CABIN DOOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05CL035Fire Detector · inoperativeCLE - THE CREW REPORTED A APU FIRE INDICATION WHILE STARTING THE APU IN FLIGHT. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE/OVERHEAT DETECTOR. OPERATIONAL CHECKS WERE GOOD.SDR C2XA05CL020Sign · inoperativeDURING ROUTINE MAINTENANCE, THE EXIT ROW EMERGENCY EXIT SIGN DID NOT ILLUMINATE DURING TESTING. MAINTENANCE REPLACED THE EXIT SIGN AND OPERATIONAL TESTS WERE GOOD.SDR C2XA05CL017Heater · burnedCLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD.SDR C2XA05CL007Engine · leakingCLE FLIGHT NR 2153, AFTER TAKEOFF, THE CREW SAW AND SMELLED SMOKE AND THE LAV SMOKE ALARM SOUNDED. THE AIRCRAFT RETURNED TO CLE WITHOUT INCIDENT. MAINTEANCE FOUND THE NR 1 ENGINE BLOWING SMOKE INTO THE AIRCRAFT. THE NR 1 ENGINE WAS REMOVED AND REPLACED. THSDR CA050107003Compressor · seized(CAN) UNCOMMANDED IN FLIGHT SHUTDOWN DURING CLIMBOUT AT APPROXIMATELY 25,000 FT. PILOT HEARD A LOUD BANG FOLLOWED BY A UNCOMMANDED SPOOL DOWN TO THE RT ENGINE. AN EMERGENCY WAS DECLARED AND A/C RETURNED TO FIELD ACCOMPLISHING A UNEVENTFUL SINGLE ENGINE LANDISDR C2XA04TY164Bulb · burned outTYS, DURING A NORMAL ROUTINE CHECK THE EMERGENCY LIGHT AT SEAT 9C WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE BULB IAW EMB 145-AMM 33-50-02. OPS CHECKED GOOD.SDR C2XA04TY109Battery · dischargedTYS - DURING A OVERNIGHT SERVICE/ROUTINE INSPECTION THE EMERGENCY LIGHT STRIP AT SEAT ROWS 7, 8 AND 9 WAS FOUND INOP. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY BATTERY AT THE NR 3 LOCATION. OPS CHECK WAS GOOD AND A/C PUT BACK IN SERVICE.SDR C2XA04CL068Uplock · brokenCLE FLT 2885 THE CREW REPORTED THE RIGHT MAIN LANDING GEAR DID NOT RETRACT. MAINTENANCE REMOVED AND REPLACED THE RT MLG UPLOCK BOX. AIRCRAFT RETURNED TO SERVICE.SDR CA040629001Engine · making metal(CAN) PRELIMINARY REPORT, HIGH OIL TEMPERATURE, LOW OIL PRESSURE AND IMPENDING BYPASS MESSAGE. PILOT COMMANDED THE IFSD DURING CRUISE. EMERGENCY DECLARED AND UNEVENTFUL LANDING. REPORTED METAL DEBRIS ON OIL TANK CHIP DETECTOR AND NOT ABLE TO ROTATE FAN OR COSDR CX2A04RI004Engine · fireCREW RETURNED ACFT TO THE GATE AFTER ENG NR 1 HUNG START AND AN ABORTED ENG NR 1 HOT START. PASSENGERS WERE DEPLANED. MAINTENANCE DISCOVERED NR 1 ENG SMOKING AND SUSPECTED ENGINE CORE FIRE. MAINTENANCE PROCEEDED WITH NR 1 ENG DRY MOTORING TO EXPEL RESIDUAL SDR C2XA04IA073Engine · malfunctionedIAH - FLIGHT 2376 THE CREW REPORTED THAT THE NUMBER ONE ENGINE SHOWED LOW OIL PRESSURE, AND HIGH OIL TEMPERATURE WITH A SMELL OF SMOKE DURING CRUISE. THE CREW SHUT DOWN THE NUMBER ONE ENGINE AS A PRECAUTION, AND LANDED AT IAH WITHOUT INCIDENT. MAINTENANCE RESDR C2XA04TY091Bulb · burned outDURING A SEVICE/ROUTINE OF A/C THE EMERGENCY LIGHT BULB WAS FOUND BLOWN OVERHEAD LEFT EMERGENCY DOOR. REPLACED BULB AND OPS CHECK WAS GOOD. A/C WAS RELEASED FOR SERVICE.SDR C2XA04CL062Proximity Sensor · dirtyCREW REPORTED THAT THE LANDING GEAR LEVER COULD NOT BE MOVED UP AFTER TAKEOFF. ALSO GOT LANDING GEAR AIR/GROUND FAIL MESSAGE ON ICAS. CREW DIVERTED TO EWR AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED SYSTEM. CLEANED CONNECTIONS ON NOSE LANDING GEAR PSDR CA040602001Blade · failed(CAN) AC YAW AND LOUD BANG IN CLIMB AT 21,000 FT. ENGINE SHUTDOWN UNCOMMANDED. EMERGENCY DECLARED AND AC DIVERTED. ON GROUND INSP FOUND THAT N1 WOULD NOT ROTATE. DISASSEMBLY OF ENG AT RRC SHOWED SEVERE TURBINE DAMAGE. SULPHIDATION, PROBABLY CAUSED THE DESDR C2XA04CL055Bulb · inoperativeDURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT AT ROW 9BC (IN PSU) WAS FOUND INOPERATIVE. MAINTENANCE REPLACED LIGHT BULB. OPERATIONAL CHECKS WERE GOOD.SDR C2XA04CL054Liner · misalignedDURING ROUTINE MAINTENANCE THE LT OVERWING EMERGENCY EXIT WOULD NOT OPEN. MAINTENANCE INSPECTED AND FOUND THE LT OVERWING INNER DOOR LINER TO BE MISALIGNED. MAINTENANCE REALIGNED LINER AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA04SH265Sill · corrodedSHV-DURING C CHECK THE LEFT SILL WAS FOUND TO BE CORRODED AFT OF FRAME 23 AND FORWARD OF FRAME 25. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH264Strap · corrodedSHV-DURING C CHECK THE AFT DIGITAL STRAP AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH263Angle · corrodedSHV-DURING C CHECK THE RIGHT RAMP ANGLE AT FRAME 20 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED ANGLE IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH260Floorbeam · corrodedSHV-DURING C CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 19. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH259Buttstrap · corrodedSHV-DURING C CHECK THE CENTER OMEGA BEAM BUTTSTRAP BETWEEN FRAME 18 AND 24 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH256Sill · corrodedSHV-DURING C CHECK THE SERVICE DOOR FORWARD SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-10. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH255Doubler · corrodedSHV-DURING C CHECK THE DOUBLER ON THE RIGHT OMEGA BEAM AT FRAME 18 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH254Strap · corrodedSHV-DURING C CHECK THE FORWARD DIGITAL STRAP BETWEEN FRAMES 14 AND 16 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH252Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR AFT SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04TY073Bracket · wornTYS - DURING A SCHEDULED 2C INSPECTION THE RIGHT PCS AILERON O/B BRACKET BUSHING WAS FOUND MIGRATING. MAINT REMOVED AND REPLACED THE RIGHT AILERON PCA ATTACH BRACKET IAW EA-2710-01017 AND 51-20-03; 51-40-02. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPOSDR C2XA04TY072Bracket · gougedTYS - DURING A SCHEDULED 2C INSPECTION THE RT AILERON PCA ATTACH BRACKET WAS FOUND GOUGED. MAINT REMOVED AND REPLACED THE AILERON PCA BRACKET PRIMED AND PAINTED IAW SRM 51-20-03 AND EA 2710-01017. ALL WORK WAS ACCOMPLISHED AND WILL BE RELEASED UPON COMPLETIOSDR C2XA04SH249Doubler · corrodedSHV - DURING C-CHECK THE RIGHT HAND OMEGA BEAM DOUBLER AT FRAME 22 WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED DOUBLER IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH248Sill · corrodedSHV - DURING C-CHECK THE LEFT HAND SILL WAS FOUND TO BE CORRODED FROM FRAME 19 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH247Buttstrap · corrodedSHV - DURING C-CHECK THE LEFT HAND OMEGA BEAM BUTTSTRAP WAS FOUND TO BE CORRODED FROM FRAME 18 TO FRAME 23. MAINTENANCE REMOVED AND REPLACED THE AFFECTED BUTTSTRAP IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH246Sill · corrodedSHV- DURING C-CHECK THE SERVICE DOOR SILL WAS FOUND TO BE CORRODED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A DOUBLER REPAIR IAW EMB 135 SRM 53-21-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04CL041Engine · failedCLE FLIGHT NR 2162 THE CREW REPORTED NR 1 ENGINE HIGH VIBRATION ON DESCENT AND AFTER LANDING REPORTED LOW OIL PRESSURE. MAINTENANCE REPLACED THE NR 1 ENGINE AND OPERATIONAL CHECKS WERE GOOD.SDR C2XA04SH244Sill · corrodedSHV- DURING C-CHECK THE CARGO DOOR CUTOUT LOWER SILL WAS FOUND TO BE CORRODED BETWEEN FRAMES 65 AND 68. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SILL IAW EMB 135 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
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